Direct measurements of turbulent skin friction on a nonadiabactic flat plate at Mach number 6.5 and comparisons with eight theories
Turbulent skin friction on nonadiabatic flat plate at Mach number 6.5
Hopkins, E. J.↗
Engineering topics
Hopkins, E. J.
Publications and source records attributed to Hopkins, E. J..
Use of Preston tubes for measuring hypersonic turbulent skin friction
Use of Preston tubes for measuring hypersonic turbulent skin friction
Hopkins, E. J.↗
Summary and correlation of skin-friction and heat-transfer data for a hypersonic turbulent boundary layer on simple shapes
Skin friction and heat transfer data for hypersonic turbulent layer on flat plates, wind tunnel wall, and cones
Hopkins, E. J.↗
Use of Preston tubes for measuring hypersonic turbulent skin friction.
Supersonic Preston tube correlations for Mach number and Reynolds number effects on hypersonic turbulent skin friction on adiabatic surfaces, simplifying correlation
Hopkins, E. J.↗
Unit Reynolds number effects on boundary-layer transition at Mach 6.
Boundary layer transition measurement on windward side of flat plate in hypersonic wind tunnel, discussing unit Reynolds number effects at Mach 6
Hopkins, E. J.↗
Aerodynamic characteristics of several cranked leading-edge wing-body combinations at Mach numbers from 0.4 to 2.94
Aerodynamic characteristics of leading-edge sweep wing-body combinations
AERODYNAMIC CHARACTERISTICS↗
Study of surface pitots for measuring turbulent skin friction at supersonic Mach numbers - Adiabatic wall
Calibration of surface pitot tubes for measuring turbulent skin friction at supersonic speeds - adiabatic wall
SKIN FRICTION↗
Comments on ''calibration of Preston tubes in supersonic flow.''
Calibration curve for Preston tubes in supersonic flow obtained by reference-temperature method
SUPERSONIC FLOW↗
Effects of Planform Variations on the Aerodynamic Characteristics of Low-Aspect-Ratio Wings with Cranked Leading Edges
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Hopkins, E. J.↗
Comparison of Full-scale Lift and Drag Characteristics of the X-15 Airplane with Wind-tunnel Results and Theory
Aerodynamic lift and drag characteristics comparison between full scale and wind tunnel model of X-15 aircraft
X-15 AIRCRAFT↗
A comparison of full-scale X-15 lift and drag characteristics with wind-tunnel results and theory
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Fetterman, D. E., Jr.↗